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(2019 BA5)
Classification: Apollo [NEO]          SPK-ID: 3838077
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2458518.5 (2019-Feb-04.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5213911407879672 0.00084181  
a 2.065226521274973 0.0036422 au
q .9884357093618497 4.6762e-06 au
i 7.205771456513226 0.0084332 deg
node 138.7496171702016 0.0016431 deg
peri 22.76240612989844 0.0029756 deg
M 352.8176463290645 0.019716 deg
tp 2458540.127895031567
(2019-Feb-25.62789503)		 0.0021561 TDB
period 1084.051630995495
2.97		 2.8678
0.007852		 d
yr
n .3320875036822818 0.0008785 deg/d
Q 3.142017333188096 0.0055413 au
   Orbit Determination Parameters
   # obs. used (total)      90  
   data-arc span      13 days  
   first obs. used      2019-01-30  
   last obs. used      2019-02-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .40957  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Feb-14 07:04:53  

Additional Information
 Earth MOID = .0203323 au 
 Jupiter MOID = 1.85008 au 
 T_jup = 3.586 
[ show covariance matrix ]

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 25.2   .46977 MPO467427 autocmod 2.6q

[ show close-approach data ]
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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